Engine Model: 15D23. Designer: KBMash. Developed in: 1961-1966. Application: RT-2 Stage 1. Propellants: Solid. Thrust(vac): 892.000 kN (200,529 lbf). Thrust(sl): 862.000 kN (193,785 lbf). Burn time: 75 sec. Diameter: 1.84 m (6.03 ft). Length: 8.70 m (28.50 ft). Chambers: 1. Country: Russia. Status: Out of Production. Three gimballed nozzles for steering. Ammonium perchlorate/aluminium propellant. Chamber pressure 40 kgf/cm2.
15D23 used on Rocket Stages
- Used on stage: 15D23. on launch vehicle: RT-2.